ADJUSTABLE DAMPER IN ANGLE OF ATTACK SENSORS
A damper assembly (22; 22A) for an angle of attack sensor (10), the damper assembly (22; 22A) comprising: a rotor (32; 32A) including a conical portion (56; 56A); a damper housing (34; 34A) in which the rotor (32; 32A) is positioned, the damper housing (34; 34A) being axially adjustable with respect...
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| creator | REID, Alexander N SCHWARTZ, Richard Alan |
| description | A damper assembly (22; 22A) for an angle of attack sensor (10), the damper assembly (22; 22A) comprising: a rotor (32; 32A) including a conical portion (56; 56A); a damper housing (34; 34A) in which the rotor (32; 32A) is positioned, the damper housing (34; 34A) being axially adjustable with respect to the rotor (32; 32A) and including a tapered interior surface (58; 58A) that matches a profile of the conical portion (56; 56A) and interior housing threading on an interior surface (58; 58A) of the damper housing (34; 34A); a body (30; 30A) having a portion positioned in the damper housing (34; 34A), the body (30; 30A) connected to the damper housing (34; 34A) to form a chamber (36; 36A) between the body (30; 30A) and the damper housing (34; 34A), wherein the rotor (32; 32A) is located within the chamber (36; 36A), and wherein the body (30; 30A) includes exterior threading (52; 52A); and a locking mechanism (50) adjacent the damper housing (34; 34A) to fix the damper housing (34; 34A) with respect to the rotor (32; 32A). |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP4019801A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP4019801A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP4019801A13</originalsourceid><addsrcrecordid>eNrjZNBxdPEKDQ5xdPJxVXBx9A1wDVLw9FNw9HMH8v3dFBxDQhydvRWCXf2C_YOCeRhY0xJzilN5oTQ3g4Kba4izh25qQX58anFBYnJqXmpJvGuAiYGhpYWBoaOhMRFKADChJHk</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>ADJUSTABLE DAMPER IN ANGLE OF ATTACK SENSORS</title><source>esp@cenet</source><creator>REID, Alexander N ; SCHWARTZ, Richard Alan</creator><creatorcontrib>REID, Alexander N ; SCHWARTZ, Richard Alan</creatorcontrib><description>A damper assembly (22; 22A) for an angle of attack sensor (10), the damper assembly (22; 22A) comprising: a rotor (32; 32A) including a conical portion (56; 56A); a damper housing (34; 34A) in which the rotor (32; 32A) is positioned, the damper housing (34; 34A) being axially adjustable with respect to the rotor (32; 32A) and including a tapered interior surface (58; 58A) that matches a profile of the conical portion (56; 56A) and interior housing threading on an interior surface (58; 58A) of the damper housing (34; 34A); a body (30; 30A) having a portion positioned in the damper housing (34; 34A), the body (30; 30A) connected to the damper housing (34; 34A) to form a chamber (36; 36A) between the body (30; 30A) and the damper housing (34; 34A), wherein the rotor (32; 32A) is located within the chamber (36; 36A), and wherein the body (30; 30A) includes exterior threading (52; 52A); and a locking mechanism (50) adjacent the damper housing (34; 34A) to fix the damper housing (34; 34A) with respect to the rotor (32; 32A).</description><language>eng ; fre ; ger</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BLASTING ; COSMONAUTICS ; ENGINEERING ELEMENTS AND UNITS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT ; LIGHTING ; MEANS FOR DAMPING VIBRATION ; MEASURING ; MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION,OR SHOCK ; MECHANICAL ENGINEERING ; PARACHUTES ; PERFORMING OPERATIONS ; PHYSICS ; SHOCK-ABSORBERS ; SPRINGS ; TESTING ; THERMAL INSULATION IN GENERAL ; TRANSPORTING ; WEAPONS</subject><creationdate>2022</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220629&DB=EPODOC&CC=EP&NR=4019801A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220629&DB=EPODOC&CC=EP&NR=4019801A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>REID, Alexander N</creatorcontrib><creatorcontrib>SCHWARTZ, Richard Alan</creatorcontrib><title>ADJUSTABLE DAMPER IN ANGLE OF ATTACK SENSORS</title><description>A damper assembly (22; 22A) for an angle of attack sensor (10), the damper assembly (22; 22A) comprising: a rotor (32; 32A) including a conical portion (56; 56A); a damper housing (34; 34A) in which the rotor (32; 32A) is positioned, the damper housing (34; 34A) being axially adjustable with respect to the rotor (32; 32A) and including a tapered interior surface (58; 58A) that matches a profile of the conical portion (56; 56A) and interior housing threading on an interior surface (58; 58A) of the damper housing (34; 34A); a body (30; 30A) having a portion positioned in the damper housing (34; 34A), the body (30; 30A) connected to the damper housing (34; 34A) to form a chamber (36; 36A) between the body (30; 30A) and the damper housing (34; 34A), wherein the rotor (32; 32A) is located within the chamber (36; 36A), and wherein the body (30; 30A) includes exterior threading (52; 52A); and a locking mechanism (50) adjacent the damper housing (34; 34A) to fix the damper housing (34; 34A) with respect to the rotor (32; 32A).</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COSMONAUTICS</subject><subject>ENGINEERING ELEMENTS AND UNITS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</subject><subject>HEATING</subject><subject>INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT</subject><subject>LIGHTING</subject><subject>MEANS FOR DAMPING VIBRATION</subject><subject>MEASURING</subject><subject>MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION,OR SHOCK</subject><subject>MECHANICAL ENGINEERING</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>SHOCK-ABSORBERS</subject><subject>SPRINGS</subject><subject>TESTING</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNBxdPEKDQ5xdPJxVXBx9A1wDVLw9FNw9HMH8v3dFBxDQhydvRWCXf2C_YOCeRhY0xJzilN5oTQ3g4Kba4izh25qQX58anFBYnJqXmpJvGuAiYGhpYWBoaOhMRFKADChJHk</recordid><startdate>20220629</startdate><enddate>20220629</enddate><creator>REID, Alexander N</creator><creator>SCHWARTZ, Richard Alan</creator><scope>EVB</scope></search><sort><creationdate>20220629</creationdate><title>ADJUSTABLE DAMPER IN ANGLE OF ATTACK SENSORS</title><author>REID, Alexander N ; SCHWARTZ, Richard Alan</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP4019801A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2022</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COSMONAUTICS</topic><topic>ENGINEERING ELEMENTS AND UNITS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</topic><topic>HEATING</topic><topic>INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT</topic><topic>LIGHTING</topic><topic>MEANS FOR DAMPING VIBRATION</topic><topic>MEASURING</topic><topic>MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION,OR SHOCK</topic><topic>MECHANICAL ENGINEERING</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>SHOCK-ABSORBERS</topic><topic>SPRINGS</topic><topic>TESTING</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>REID, Alexander N</creatorcontrib><creatorcontrib>SCHWARTZ, Richard Alan</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>REID, Alexander N</au><au>SCHWARTZ, Richard Alan</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>ADJUSTABLE DAMPER IN ANGLE OF ATTACK SENSORS</title><date>2022-06-29</date><risdate>2022</risdate><abstract>A damper assembly (22; 22A) for an angle of attack sensor (10), the damper assembly (22; 22A) comprising: a rotor (32; 32A) including a conical portion (56; 56A); a damper housing (34; 34A) in which the rotor (32; 32A) is positioned, the damper housing (34; 34A) being axially adjustable with respect to the rotor (32; 32A) and including a tapered interior surface (58; 58A) that matches a profile of the conical portion (56; 56A) and interior housing threading on an interior surface (58; 58A) of the damper housing (34; 34A); a body (30; 30A) having a portion positioned in the damper housing (34; 34A), the body (30; 30A) connected to the damper housing (34; 34A) to form a chamber (36; 36A) between the body (30; 30A) and the damper housing (34; 34A), wherein the rotor (32; 32A) is located within the chamber (36; 36A), and wherein the body (30; 30A) includes exterior threading (52; 52A); and a locking mechanism (50) adjacent the damper housing (34; 34A) to fix the damper housing (34; 34A) with respect to the rotor (32; 32A).</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
| recordid | cdi_epo_espacenet_EP4019801A1 |
| source | esp@cenet |
| subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COSMONAUTICS ENGINEERING ELEMENTS AND UNITS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT LIGHTING MEANS FOR DAMPING VIBRATION MEASURING MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION,OR SHOCK MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS PHYSICS SHOCK-ABSORBERS SPRINGS TESTING THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS |
| title | ADJUSTABLE DAMPER IN ANGLE OF ATTACK SENSORS |
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